Asymptotic behavior of hypersonic flow over blunted slender wedges.
- 1 November 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (11) , 2235-2236
- https://doi.org/10.2514/3.4979
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- UNIRED THEORY FOR THE BENDING AND BUCKLING OF SANDWICH SHELLS - APPLICATION TO AXIALLY COMPRESSED CIRCULAR CYLINTRICAL SHELLSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Theory for Moderately Large Deflections of Thin Sandwich ShellsJournal of Applied Mechanics, 1965
- Sandwich Shells of Arbitrary ShapeJournal of Applied Mechanics, 1964
- Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic FlowJournal of the Aerospace Sciences, 1961
- INTRODUCTIONPublished by Elsevier ,1961
- Introduction to Hypersonic FlowPublished by Elsevier ,1961